R 1EFF : 106-149, 155-199, 208-299, 301-399, 1 31-32-00Page A38 1401-499, 1Aug 01/05 1 1 1CES 1

 --
CURRENT LEG REPORT CURRENT LEG ECAM REPOR T | | In normal operation
 --
--
GMT/DATE INIT  | |  Item added in the event of clockfailure, plus long power cutoff.
 --
--
PFR FILTER PROGRAM  || | | | Filter printing
 --
(Ref. Fig. 027)

 These different maintenance reports are transmitted by the CFDIU to the MCDU and they are principally intended for line maintenance.

R **ON A/C 106-149, 155-199, 208-299, 301-399, 401-499,
 In flight the menu is:
 1EFF : ALL 1 31-32-00Page A39 1 1 Aug 01/05 1 1 1CES 1

 CFDIU - CFDS Menu in Flight
 Figure 027

R 1EFF : 001-049, 051-099, 101-105, 151-154, 1 31-32-00Page A40 1201-207, 1May 01/05 1 1 1CES 1 (Ref. Fig. 027A)

 --
CURRENT LEG REPORT CURRENT LEG ECAM REPORT CURRENT FLIGHT REPORT  || | -- In normal operation
 --
GMT/DATE INIT  | | -- Item added in the event of clockfailure, plus long power cutoff.
 --
REPORTS PROGRAMMING (IF ACARS MU or ATSU INSTALLED)  || | | -- ACARS MU (or ATSU) programmingand printing functions programming
 --
PFR FILTER PROGRAM  || | -- Filter printing
 --
PASSWORD CHANGE  | | -- Password modification

 These different maintenance reports are transmitted by the CFDIU to the MCDU and they are principally intended for line maintenance.
 **ON A/C ALL
 (1) Description of CFDIU reports
 (a) LAST/CURRENT LEG REPORT (Ref. Fig. 028) The purpose of this item, which is part of the main maintenance menu, is to present, in flight or on the ground, the internal fault messages (class 1 and 2), concerning all systems, occured during the last or the current flight, and the list of systems affected by this fault that are called identifiers. Capacity : 40 failures. These messages contain the text of the internal fault i.e. the faulty LRU and its ATA reference, associated with the time at which the fault occurred and the flight phase during which it occurred.
R 1EFF : ALL 1 31-32-00Page A41 1 1 May 01/05 1 1 1CES 1

 CFDIU - CFDS Menu in Flight
 Figure 027A

R 1EFF : 106-149, 155-199, 208-299, 301-399, 1 31-32-00Page A42 1401-499, 1Aug 01/05 1 1 1CES 1

 CFDIU - LAST (or CURRENT) LEG REPORT Figure 028
 1EFF : 1 1R 1CES  ALL  1 11 1 31-32-00 Page A43 May 01/05

 The date is entered in the header.
 Access to the identifiers can be gained by pressing the line key
 adjacent to the fault, so as to help identification of the fault.
 This information is displayed on the MCDU in clear when this
 function is activated by the operator.
 On the ground, the item is presented under the title LAST LEG
 REPORT, in flight it is presented under the title CURRENT LEG
 REPORT.

 (b)
 LAST/CURRENT LEG ECAM REPORT (Ref. Fig. 029) The purpose of this item, which is part of the main maintenance menu, is to present, in flight or on the ground, the warning messages (class 1 and 2 faults) displayed on the upper ECAM display unit during the last or the current flight. These are the primary or independent warnings. When several identical and consecutive warnings are transmitted, the CFDIU memorizes the first occurence only and carries out counting with a maximum of 8. Capacity: 40 warnings. These messages contain the ECAM warning associated with its ATA reference, the time and the flight phase at which the fault occurred. The date is entered in the header. This information is displayed on the MCDU in clear when this function is activated by the operator. On the ground, the item is presented under the title LAST LEG ECAM REPORT, in flight it is presented under the title CURRENT LEG ECAM REPORT.

 (c)
 PREVIOUS LEGS REPORT (Ref. Fig. 030) The purpose of this item, which is part of the main maintenance menu, is to present, on the ground only, the internal fault messages (class 1 and 2) concerning all systems, appeared during the previous 64 flights (fault history). This item is the "sum" of LAST LEG REPORT items over several flights. These fault messages contain the names of the LRUs affected by a fault associated with the time and date at which the fault occurred, the flight phase during which it occurred, the flight number (0 to 63) and the ATA references of the faulty systems. Aircraft identification is entered in the header. This information is displayed on the MCDU in clear when this function is activated by the operator.

 1EFF : ALL 1 31-32-00Page A44 1 1 May 01/05R 1 1 1CES 1

 CFDIU - LAST (or CURRENT) LEG ECAM REPORT Figure 029
　
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